US6007024A - Safety device for a container disposed in the interior of an aircraft - Google Patents

Safety device for a container disposed in the interior of an aircraft Download PDF

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Publication number
US6007024A
US6007024A US08/724,785 US72478596A US6007024A US 6007024 A US6007024 A US 6007024A US 72478596 A US72478596 A US 72478596A US 6007024 A US6007024 A US 6007024A
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US
United States
Prior art keywords
container
belt
deflecting element
aircraft
force deflecting
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US08/724,785
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English (en)
Inventor
Walter Anton Stephan
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Facc AG
Original Assignee
Fischer Advanced Composite Components AG
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Application filed by Fischer Advanced Composite Components AG filed Critical Fischer Advanced Composite Components AG
Assigned to FISCHER ADVANCED COMPOSTIE COMPONENTS GESELLSCHAFT M.B.H. reassignment FISCHER ADVANCED COMPOSTIE COMPONENTS GESELLSCHAFT M.B.H. ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: STEPHAN, WALTER A.
Application granted granted Critical
Publication of US6007024A publication Critical patent/US6007024A/en
Assigned to FISCHER ADVANCED COMPOSITE COMPONENTS AG reassignment FISCHER ADVANCED COMPOSITE COMPONENTS AG ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: FISCHER ADVANCED COMPOSITE COMPONENTS GESELLSCHAFT M.B.H.
Assigned to FACC AG reassignment FACC AG CHANGE OF NAME (SEE DOCUMENT FOR DETAILS). Assignors: FISCHER ADVANCED COMPOSITE COMPONENTS GESELLSCHAFT M.B.H.
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
    • B64D11/003—Stowage devices for passengers' personal luggage

Definitions

  • This invention relates to a device for protecting passengers from injury in the case of overstressing of the "overhead stowage containers" disposed in the interior of aircraft, more particularly above the passengers, and to a container for the aircraft industry having a device of the kind specified.
  • baggage stowage containers with relatively heavy baggage, so that the actual weight of baggage in the baggage stowage containers can be quite high.
  • an emergency for example, an emergency landing the items of baggage may turn into dangerous projectiles.
  • the baggage stowage containers may remain undamaged, but their supports are damaged and the baggage storage containers and its contents may drop onto the passengers.
  • Other containers used on board aircraft are also being utilised to an ever increasing extent such as, for example, trolleys taking refreshments and beverages to the passengers.
  • An object of the invention is to provide a device which ensures the maximum possible passenger safety in emergency situations when the containers, mainly overhead stowage containers used inside the aircraft become overloaded or overstressed. Another object is to provide a container which also ensures such safety.
  • the construction according to the invention ensures maximum passenger safety by sharing out the task between the conventional container suspension and the safety device.
  • Any manner of fixing the container, even merely a temporary attachment to any place on the fuselage, is considered to be a suspension.
  • a conventional suspension is free from forces and clearance, while the force deflecting element of the safety device can be attached to existing or newly created points of suspension on the fuselage, a freedom of movement of up to a few millimetres being permitted.
  • the force deflecting element deflects the inertia forces of the base plate, side walls or doors of the container into the supporting construction of the aircraft.
  • the number of force deflecting elements and the points of attachment can be adapted to the maximum acceleration anticipated.
  • FIG. 1 a diagrammatic side elevation of two containers in a row of overhead stowage containers
  • FIG. 1a a section, taken along the line 1a--1a in FIG. 1.
  • FIG. 1b a variant of the embodiment shown in FIG. 1 having only one belt
  • FIG. 2 a detail of a belt portion designed to absorb kinetic energy
  • FIG. 3 a section of a variant attachment of the safety device according to the invention to the fuselage
  • FIG. 4a an end view of the passenger compartment of an aircraft during normal flying operation, the overhead stowage containers shown in the left-hand part A having the safety device according to the invention, those in the right-hand part D having no such device, and
  • FIG. 4b the view shown in FIG. 4a after loading due to an emergency, for example, a crash.
  • FIG. 1 shows two overhead stowage containers 2, a row of which its provided on both sides of the passenger compartment substantially along its entire length.
  • FIG. 1a shows a portion of a fuselage 1 to which the overhead stowage container 2 according to the invention is secured.
  • the inherently strong base plate 2a of the stowage containers 2 is reinforced by longitudinally extending struts 3 which take the form of aluminum sections which can also carry the oxygen supply and further lines or additional units.
  • Secured preferably to the base plate 2a rigidly or, for example, releasably by screwed connection, bayonet-type connections or the like are two belts 4 which inhibit the stowage container 2 dropping onto the passengers in an emergency, after the failure of the conventional suspension systems.
  • the number and construction of the belts can be adapted to the maximum acceleration to be intercepted.
  • the belt(s) 4 extend along the stowage container wall, being deflected around corners or rounded portions of the stowage container 2, from the reinforced base plate 2a (advantageously from the mechanically most stable portion of the container) to a place of attachment 5.
  • the stowage containers 2 are also suspended via the conventional attaching straps or bolts.
  • the flexibility of the force deflecting element is particularly important for deflections around corners or rounded portions of the stowage container 2, to enable the length to be changed in as unimpeded and space saving a manner as possible.
  • the places of attachment 5 are suspended via supporting elements 6 from points of articulation 7 on the fuselage 1.
  • a tear-resistant, force-deflecting belt 4 has a suspension plate 41 attached to a sewn strap of the belt.
  • the belt 4 is suspended with only slight freedom of movement from the place of attachment 5 of the storage container 2 or from a separate place of attachment for the safety device according to the invention. If a tensile loading limit determined by the materials and structure of the belt is exceeded, a preferably irreversible change in the length of the belt absorbs kinetic energy and, in a manner similar to a safety belt in a motor vehicle, inhibits the stowage containers 2 from dropping onto the passengers' heads (see FIG. 4b part B).
  • the stowage containers can withstand loadings up to 16 times and 20 times terrestrial acceleration (16 g to 20 g), without the stowage container having to be designed mechanically for such stressing in the zone of its points of suspension, something which would moreover substantially increase its weight. Under such loadings conventional attaching and suspension systems would almost certainly tear away or fail.
  • the force deflecting element 4 has a device 42 for absorbing kinetic energy.
  • this device is formed, for example, by a S-shaped or Z-shaped superimposed belt portion which is fixed in this configuration by seams 43.
  • the seams 43 are designed to tear open under a predetermined loading, thereby absorbing energy while the operative portion of the belt 4 increases in length (see FIG. 4b, part A). In an emergency such a lengthening of the belt 4 and the associated lowering of the stowage container 2 by approximately 2 to 3 cm can be tolerated.
  • a hole 44 in the suspension plate 41 is used for suspension from or connection to the points of articulation 7 on the fuselage 1.
  • the stowage container 2 can also be wrapped in a UD fabric and be provided with suitable straps for suspension from the fuselage.
  • the safety device according to the invention increases the weight of the stowage container by only approximately 3 to 4 while a similar reinforcement of the places of attachment and the suspension devices would cause a weight increase of approximately 20%.
  • FIG. 3 shows in section a detail of the invention at the place of attachment 5.
  • the place of attachment 5 takes the form of a strap which is disposed on the fuselage 1.
  • a bush 21 is inserted in the side wall of the stowage container 2 in conventional manner and without any specially reinforced construction and is glued or connected in some other manner to said wall.
  • the baggage stowage container 2 is suspended from the fuselage 1 via a pin 8 which extends through an opening in the strap, representing the place of attachment 5 and the bush 21.
  • the belt 4 is also attached to the strap 5, the pin 8 also extending through the opening 44. In an extreme case of stressing the bush 21 will tear open, while the highly stabily constructed and located strap remains intact and therefore the belt 4 also holds.
  • the belt 4 After the belt 4 has been lengthened by the device for absorbing kinetic energy, it retains the stowage container 2 securely above the passengers' heads (see FIG. 4a, part A). If the strap is not very stably constructed, additional places of attachment can also be provided for the safety device according to the invention and the safety device part of the container 2; there is a relatively considerable freedom as regards the arrangement and number of such places of attachment.

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Emergency Lowering Means (AREA)
  • Vehicle Step Arrangements And Article Storage (AREA)
  • Sealing Devices (AREA)
  • Package Frames And Binding Bands (AREA)
  • Portable Outdoor Equipment (AREA)
  • Load-Engaging Elements For Cranes (AREA)
  • Helmets And Other Head Coverings (AREA)
  • Passenger Equipment (AREA)
  • Air Bags (AREA)
US08/724,785 1995-10-04 1996-10-03 Safety device for a container disposed in the interior of an aircraft Expired - Lifetime US6007024A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
AT0164895A AT402389B (de) 1995-10-04 1995-10-04 Sicherheitsvorrichtung für im flugzeuginnenraum angebrachte behälter sowie behälter für die luftfahrtindustrie
AT1648/95 1995-10-04

Publications (1)

Publication Number Publication Date
US6007024A true US6007024A (en) 1999-12-28

Family

ID=3517971

Family Applications (1)

Application Number Title Priority Date Filing Date
US08/724,785 Expired - Lifetime US6007024A (en) 1995-10-04 1996-10-03 Safety device for a container disposed in the interior of an aircraft

Country Status (8)

Country Link
US (1) US6007024A (es)
EP (1) EP0767100B1 (es)
CN (1) CN1088673C (es)
AT (2) AT402389B (es)
CA (1) CA2186981C (es)
DE (1) DE59609643D1 (es)
ES (1) ES2181864T3 (es)
SG (1) SG40892A1 (es)

Cited By (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6149102A (en) * 1998-03-25 2000-11-21 Robertson Aviation Llc Mounting system for auxiliary fuel tank
US6270221B1 (en) 1998-08-19 2001-08-07 Alcon Universal Ltd. Apparatus and method for measuring vision defects of a human eye
US20050040287A1 (en) * 2001-10-09 2005-02-24 Stephan Walter Alfred Overhead luggage container, particularly for airplanes
US6883753B1 (en) * 2004-03-25 2005-04-26 The Boeing Company Overhead bin and monument attachment support system
US20060086886A1 (en) * 2004-08-31 2006-04-27 Airbus Deutschland Gmbh Mounting device for interior equipment in aircraft
US20060091257A1 (en) * 2004-11-01 2006-05-04 Melberg David S Modular vehicle units, including aircraft interior storage units, and associated methods
US20070084966A1 (en) * 2005-10-14 2007-04-19 Haynes Michael S Stowage bin with shear fittings
US20080277527A1 (en) * 2005-11-17 2008-11-13 Airbus Deutschland Gmbh Attachment structure for affixing interior equipment components of an aircraft passenger cabin
US20090026318A1 (en) * 2007-07-11 2009-01-29 Airbus Deutschland Gmbh Installation system for an airplane
US20090301832A1 (en) * 2006-02-15 2009-12-10 Airbus Deutschland Gmbh Energy Absorber for Aircraft
US20100051401A1 (en) * 2006-02-15 2010-03-04 Airbus Deutschland Gmbh Force level control for an energy absorber for aircraft
US20110062284A1 (en) * 2005-10-14 2011-03-17 The Boeing Company Stowage bin with shear fittings
US20110084166A1 (en) * 2008-05-28 2011-04-14 Airbus Operations Gmbh Arrangement for dividing a space into a plurality of areas
US20120167283A1 (en) * 2010-12-31 2012-07-05 Hallett Mark B Strap shock absorber
US20120223184A1 (en) * 2010-07-10 2012-09-06 Diehl Aircabin Gmbh Device for supplying loads in the overhead area of a passenger cabin, in particular in commercial aircraft
US20120228425A1 (en) * 2009-10-30 2012-09-13 Airbus Operations Gmbh Storage compartment module with an integrated supply channel for optimized installation
US20120312921A1 (en) * 2009-12-18 2012-12-13 Grosse-Plankermann Peter System component module and method for mounting a system component module
US20130249365A1 (en) * 2012-03-26 2013-09-26 Diehl Aerospace Gmbh Luggage storage compartment, aircraft with a luggage storage compartment, and method for operating the luggage storage compartment
US20140152159A1 (en) * 2011-07-29 2014-06-05 Airbus Operations Gmbh Supporting structure for moveable bin
US10318904B2 (en) 2016-05-06 2019-06-11 General Electric Company Computing system to control the use of physical state attainment of assets to meet temporal performance criteria

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4325195A (en) * 1978-05-16 1982-04-20 The Toro Company Snow thrower
DE19633469C1 (de) * 1996-08-20 1997-09-04 Daimler Benz Aerospace Airbus Vorrichtung zum Halten von Ausrüstungsteilen im oberen Bereich von Passagierkabinen, insbesondere von Gepäckablagen in Flugzeugpassagierkabinen
AT413812B (de) * 2001-10-17 2006-06-15 Fischer Adv Components Gmbh Aufhängevorrichtung für absenkbare gebäckablagebehälter
CN1317861C (zh) * 2003-07-21 2007-05-23 中兴通讯股份有限公司 无线局域网接入点设备虚拟局域网的实现方法
DE102004049700B4 (de) * 2004-10-12 2007-10-18 Aircabin Gmbh Kraftunterstützungsvorrichtung mit lastabhängiger Kraftunterstützung
FR2888561B1 (fr) * 2005-07-12 2008-10-31 Airbus Groupement D Interet Ec Cloison de separation dans une cabine d'aeronef
US10793277B2 (en) * 2017-03-10 2020-10-06 The Boeing Company Electronic stowage bin control systems and methods

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US2735377A (en) * 1956-02-21 Cargo tie-down
US3377044A (en) * 1966-03-02 1968-04-09 Zelm Associates Inc Van Cargo tie-down apparatus
DE1278850B (de) * 1964-05-15 1968-09-26 R L Lambin & Ravau Sa Stossdaempfer fuer Sicherheitsgurte und Fallschirme
US4125302A (en) * 1976-05-04 1978-11-14 Peritz Leigh A Easy-leveling support device
GB2169256A (en) * 1985-01-08 1986-07-09 Grigory Dmitrievich Sukhover Aircraft cabin
US5080453A (en) * 1990-12-24 1992-01-14 Miller Guy D Utility cabinet for mounting on sloping walls
US5108048A (en) * 1989-09-15 1992-04-28 The Boeing Company Stowage bin and support panel system for convertible aircraft and method of installation
US5131620A (en) * 1991-03-18 1992-07-21 Westinghouse Electric Corp. Rack for suspending a component below a support surface
EP0514957A1 (en) * 1991-05-24 1992-11-25 The Boeing Company Detachable storage bin system
EP0557267A1 (de) * 1992-02-20 1993-08-25 FISCHER ADVANCED COMPOSITE COMPONENTS GESELLSCHAFT m.b.H. Kunststoffbehälter
US5377856A (en) * 1993-03-29 1995-01-03 Brierton; Dennis M. Air cargo security vault
US5395074A (en) * 1993-03-10 1995-03-07 Health Tecna Aerospace Company A Unit Of Ciba-Geigy Retrofit bezel assembly
US5549258A (en) * 1994-12-23 1996-08-27 Heath Tecna Aerospace Company Retrofit luggage bin assembly compatible with existing aircraft bin supports

Patent Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2735377A (en) * 1956-02-21 Cargo tie-down
DE1278850B (de) * 1964-05-15 1968-09-26 R L Lambin & Ravau Sa Stossdaempfer fuer Sicherheitsgurte und Fallschirme
US3377044A (en) * 1966-03-02 1968-04-09 Zelm Associates Inc Van Cargo tie-down apparatus
US4125302A (en) * 1976-05-04 1978-11-14 Peritz Leigh A Easy-leveling support device
GB2169256A (en) * 1985-01-08 1986-07-09 Grigory Dmitrievich Sukhover Aircraft cabin
US5108048A (en) * 1989-09-15 1992-04-28 The Boeing Company Stowage bin and support panel system for convertible aircraft and method of installation
US5080453A (en) * 1990-12-24 1992-01-14 Miller Guy D Utility cabinet for mounting on sloping walls
US5131620A (en) * 1991-03-18 1992-07-21 Westinghouse Electric Corp. Rack for suspending a component below a support surface
EP0514957A1 (en) * 1991-05-24 1992-11-25 The Boeing Company Detachable storage bin system
EP0557267A1 (de) * 1992-02-20 1993-08-25 FISCHER ADVANCED COMPOSITE COMPONENTS GESELLSCHAFT m.b.H. Kunststoffbehälter
US5395074A (en) * 1993-03-10 1995-03-07 Health Tecna Aerospace Company A Unit Of Ciba-Geigy Retrofit bezel assembly
US5377856A (en) * 1993-03-29 1995-01-03 Brierton; Dennis M. Air cargo security vault
US5549258A (en) * 1994-12-23 1996-08-27 Heath Tecna Aerospace Company Retrofit luggage bin assembly compatible with existing aircraft bin supports

Cited By (39)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6149102A (en) * 1998-03-25 2000-11-21 Robertson Aviation Llc Mounting system for auxiliary fuel tank
US6270221B1 (en) 1998-08-19 2001-08-07 Alcon Universal Ltd. Apparatus and method for measuring vision defects of a human eye
CN100404373C (zh) * 2001-10-09 2008-07-23 菲舍尔高级合成元件股份公司 用于飞机的高架行李存放箱
US7097138B2 (en) * 2001-10-09 2006-08-29 Fisher Advanced Composite Components Ag Overhead luggage container, particularly for airplanes
US20050040287A1 (en) * 2001-10-09 2005-02-24 Stephan Walter Alfred Overhead luggage container, particularly for airplanes
US6883753B1 (en) * 2004-03-25 2005-04-26 The Boeing Company Overhead bin and monument attachment support system
US20060086886A1 (en) * 2004-08-31 2006-04-27 Airbus Deutschland Gmbh Mounting device for interior equipment in aircraft
US7527221B2 (en) 2004-08-31 2009-05-05 Airbus Deutschland Gmbh Mounting device for interior equipment in aircraft
US20060091257A1 (en) * 2004-11-01 2006-05-04 Melberg David S Modular vehicle units, including aircraft interior storage units, and associated methods
US7309045B2 (en) * 2004-11-01 2007-12-18 The Boeing Company Modular vehicle units, including aircraft interior storage units, and associated methods
US20070084966A1 (en) * 2005-10-14 2007-04-19 Haynes Michael S Stowage bin with shear fittings
US7832685B2 (en) 2005-10-14 2010-11-16 The Boeing Company Stowage bin with shear fittings
US8047468B2 (en) 2005-10-14 2011-11-01 The Boeing Company Stowage bin with shear fittings
US20110062284A1 (en) * 2005-10-14 2011-03-17 The Boeing Company Stowage bin with shear fittings
US20090321566A1 (en) * 2005-10-14 2009-12-31 The Boeing Company Stowage Bin with Shear Fittings
US20080277527A1 (en) * 2005-11-17 2008-11-13 Airbus Deutschland Gmbh Attachment structure for affixing interior equipment components of an aircraft passenger cabin
US8403266B2 (en) 2005-11-17 2013-03-26 Airbus Operations Gmbh Attachment structure for affixing interior equipment components of an aircraft passenger cabin
US20100051401A1 (en) * 2006-02-15 2010-03-04 Airbus Deutschland Gmbh Force level control for an energy absorber for aircraft
US20090301832A1 (en) * 2006-02-15 2009-12-10 Airbus Deutschland Gmbh Energy Absorber for Aircraft
US8573372B2 (en) 2006-02-15 2013-11-05 Airbus Operations Gmbh Force level control for an energy absorber for aircraft
US8662265B2 (en) 2006-02-15 2014-03-04 Airbus Operations Gmbh Energy absorber for aircraft
US8528859B2 (en) * 2007-07-11 2013-09-10 Airbus Operations Gmbh Installation system for an airplane
US20090026318A1 (en) * 2007-07-11 2009-01-29 Airbus Deutschland Gmbh Installation system for an airplane
US20110084166A1 (en) * 2008-05-28 2011-04-14 Airbus Operations Gmbh Arrangement for dividing a space into a plurality of areas
US8613407B2 (en) 2008-05-28 2013-12-24 Airbus Operations Gmbh Assembly for separating a space into multiple areas
US8430358B2 (en) * 2009-10-30 2013-04-30 Airbus Operations Gmbh Storage compartment module with an integrated supply channel for optimized installation
US20120228425A1 (en) * 2009-10-30 2012-09-13 Airbus Operations Gmbh Storage compartment module with an integrated supply channel for optimized installation
US20120312921A1 (en) * 2009-12-18 2012-12-13 Grosse-Plankermann Peter System component module and method for mounting a system component module
US9156554B2 (en) * 2009-12-18 2015-10-13 Airbus Operations Gmbh System component module and method for mounting in an aircraft cabin
US8500065B2 (en) * 2010-07-10 2013-08-06 Diehl Aircabin Gmbh Device for supplying loads in the overhead area of a passenger cabin, in particular in commercial aircraft
US20120223184A1 (en) * 2010-07-10 2012-09-06 Diehl Aircabin Gmbh Device for supplying loads in the overhead area of a passenger cabin, in particular in commercial aircraft
US20120167283A1 (en) * 2010-12-31 2012-07-05 Hallett Mark B Strap shock absorber
US8984721B2 (en) * 2010-12-31 2015-03-24 Concussion Resources, Llc Strap shock absorber
US20140152159A1 (en) * 2011-07-29 2014-06-05 Airbus Operations Gmbh Supporting structure for moveable bin
US9511863B2 (en) * 2011-07-29 2016-12-06 Airbus Operations Gmbh Supporting structure for moveable bin
US20130249365A1 (en) * 2012-03-26 2013-09-26 Diehl Aerospace Gmbh Luggage storage compartment, aircraft with a luggage storage compartment, and method for operating the luggage storage compartment
US8955802B2 (en) * 2012-03-26 2015-02-17 Diehl Aircabin Gmbh Luggage storage compartment, aircraft with a luggage storage compartment, and method for operating the luggage storage compartment
US10318904B2 (en) 2016-05-06 2019-06-11 General Electric Company Computing system to control the use of physical state attainment of assets to meet temporal performance criteria
US10318903B2 (en) 2016-05-06 2019-06-11 General Electric Company Constrained cash computing system to optimally schedule aircraft repair capacity with closed loop dynamic physical state and asset utilization attainment control

Also Published As

Publication number Publication date
DE59609643D1 (de) 2002-10-17
AT402389B (de) 1997-04-25
ATA164895A (de) 1996-09-15
CA2186981C (en) 2005-11-29
EP0767100B1 (de) 2002-09-11
CN1152525A (zh) 1997-06-25
ATE223833T1 (de) 2002-09-15
CN1088673C (zh) 2002-08-07
CA2186981A1 (en) 1997-04-05
EP0767100A1 (de) 1997-04-09
SG40892A1 (en) 1997-06-14
ES2181864T3 (es) 2003-03-01

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